From 980d5e20600efae6cce12589f2eee5682bdd82df Mon Sep 17 00:00:00 2001
From: Luca Miguel <luca.miguel@usp.br>
Date: Tue, 25 Jul 2023 16:31:02 +0200
Subject: [PATCH] Removed unnecessary file

---
 plot.py | 130 --------------------------------------------------------
 1 file changed, 130 deletions(-)
 delete mode 100644 plot.py

diff --git a/plot.py b/plot.py
deleted file mode 100644
index b872307..0000000
--- a/plot.py
+++ /dev/null
@@ -1,130 +0,0 @@
-from rocket_twin.systems import Station, ControllerFMU
-from cosapp.drivers import RungeKutta, NonLinearSolver
-from cosapp.recorders import DataFrameRecorder
-from cosapp.utils import swap_system
-import numpy as np
-import matplotlib.pyplot as plt
-
-model_path = r"systems\control\controller.mo"
-model_name = "controller"
-
-model_path_r = r"systems\control\rocket_controller.mo"
-model_name_r = "rocket_controller"
-
-sys = Station("sys")
-swap_system(
-    sys.controller,
-    ControllerFMU("controller", model_path=model_path, model_name=model_name),
-)
-swap_system(
-    sys.rocket.controller,
-    ControllerFMU("controller", model_path=model_path_r, model_name=model_name_r),
-)
-
-sys.connect(sys.controller.inwards, sys.rocket.inwards, ["weight_max", "weight_p"])
-sys.rocket.connect(
-    sys.rocket.controller.inwards, sys.rocket.tank.inwards, ["weight_max", "weight_p"]
-)
-
-driver = sys.add_driver(RungeKutta(order=4, time_interval=[0, 25], dt=0.01))
-solver = driver.add_child(NonLinearSolver('solver'))
-init = {"g_tank.weight_p": 10.0, "rocket.tank.weight_p": 0.0}
-values = {
-    "g_tank.w_out_max": 1.0,
-    "rocket.tank.w_out_max": 0.5,
-    "controller.time_int": 10.,
-    "rocket.controller.time_int": 10.,
-}
-
-includes = ["rocket.tank.weight_p", "g_tank.weight_p", "rocket.a"]
-
-driver.set_scenario(init=init, values=values)
-driver.add_recorder(DataFrameRecorder(includes=includes), period=1.0)
-
-sys.run_drivers()
-data = driver.recorder.export_data()
-
-time = np.asarray(data['time'])
-g_mass = np.asarray(data["g_tank.weight_p"])
-r_mass = np.asarray(data["rocket.tank.weight_p"])
-acel = np.asarray(data['rocket.a'])
-
-plt.plot(time, g_mass, label="Ground tank fuel mass")
-plt.plot(time, r_mass, label="Rocket tank fuel mass")
-plt.title("Ground and rocket fuel masses over time")
-plt.xlabel("Time (s)")
-plt.ylabel("Mass (kg)")
-plt.legend()
-plt.show()
-
-plt.plot(time, acel, label="Rocket acceleration")
-plt.title("Rocket acceleration over time")
-plt.xlabel("Time (s)")
-plt.ylabel("Acceleration (m/s²)")
-plt.legend()
-plt.show()
-
-from cosapp.base import System
-
-from rocket_twin.systems import Dynamics, Stage
-
-
-class Rocket(System):
-    """A simple model of a rocket.
-
-    Inputs
-    ------
-    n_stages: int,
-        how many stages the rocket has
-    flying: boolean,
-        whether the rocket is already flying or still on ground
-
-    Outputs
-    ------
-    """
-
-    def setup(self):
-
-
-        self.add_inward("n_stages", 1, desc="Number of rocket stages", unit='')
-
-        forces, weights, centers = ([] for i in range(self.n_stages))
-
-        for i in range(self.n_stages):
-            self.add_child(Stage(f"stage_{i}"))
-            forces[i] = f"thrust_{i}"
-            weights[i] = f"weight_{i}"
-            centers[i] = f"center_{i}"
-
-        self.add_child(
-            Dynamics(
-                "dyn",
-                forces=forces,
-                weights=weights,
-                centers=centers,
-            ),
-            pulling=["a"],
-        )
-
-        for stage in self.children:
-            if stage != "dyn":
-                self.connect(
-                    self.stage.outwards,
-                    self.dyn.inwards,
-                    {"force": f"thrust_{i}", "weight": f"weight_{i}", "center": f"center_{i}"},
-                )
-
-        
-        self.add_inward_modevar(
-            "flying", False, desc="Whether the rocket is flying or not", unit=""
-        )
-
-        self.add_event("Takeoff", trigger="dyn.a > 0")
-
-    def compute(self):
-        self.a *= self.flying
-
-    def transition(self):
-
-        if self.Takeoff.present:
-            self.flying = True
\ No newline at end of file